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The design and analysis of high hub‑tip ratio underground gas storage compressor stages
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Lixin YAO, Wei PEI, Jian CHENG, Shangming JI, Lin PEI, Xiao TAI, Yongrui SUN, Yang GUO
Fluid Machinery | 2025, 53(7) : 61 - 68
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Fluid Machinery | 2025, 53(7): 61-68
The design and analysis of high hub‑tip ratio underground gas storage compressor stages
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Lixin YAO, Wei PEI, Jian CHENG, Shangming JI, Lin PEI, Xiao TAI, Yongrui SUN, Yang GUO
Affiliations
  • ShenGu Group Co.,Ltd.,Shenyang 110869,China
Published: 2025-07-30 doi: 10.3969/j.issn.1005-0329.2025.07.009
Outline
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A large hub to hub ratio model stage is proposed to address the issue of the existing conventional hub to hub ratio model stage for domestic compressors being unable to meet the rotor stability requirements of the seven stage two‑stage scheme and can only adopt a dual cylinder design.Based on the medium hub‑tip ratio model stage of a double‑cylinder gas storage compressor,the design and development of a high hub‑tip ratio model stage has been completed by combining the forward design method,automatic optimization method and test method.The geometry,macroscopic performance,and internal flow field characteristics of different hub‑tip ratio model stages were also compared and analyzed,and it revealed the flow characteristics of the high hub‑tip ratio model stage.The study shows that the polytropic efficiency of the 0.46 high hub‑tip ratio model stage is 4.3% lower than that of the 0.39 hub‑tip ratio model stage,and the efficiency drop of the impeller part is the largest,accounting for 67.4% of the efficiency drop of the whole model stage.Adjusting the blade profile,the number of blades,and reducing the Mach number inside the impeller and the bladeless diffuser have a greater potential to improve the efficiency of the model stage.The deviation of the efficiency between the CFD and the experimental results is all within 3%,which has strong reference value.The developed model stage hub ratio has been increased by 18%,which solves the rotor stability problem of the seven‑stage two‑section scheme and realizes the design and development of a single‑cylinder gas storage compressor with a small floor area.This study addresses the stability issues of single‑cylinder seven‑stage two‑stage rotors,and fills the research gap in the application of large wheel hub ratio compressors in China,and provides valuable reference significance for the aerodynamic design,development and application of the high hub‑tip ratio model of centrifugal compressors.

gas storage  /  compressor  /  model stage  /  hub‑tip ratio  /  low specific speed
么立新, 裴威, 程健, 吉尚明, 裴林, 邰骁, 孙永瑞, 郭杨. 大轮毂比储气库压缩机模型级开发与分析. 流体机械, 2025 , 53 (7) : 61 -68 . DOI: 10.3969/j.issn.1005-0329.2025.07.009
Lixin YAO, Wei PEI, Jian CHENG, Shangming JI, Lin PEI, Xiao TAI, Yongrui SUN, Yang GUO. The design and analysis of high hub‑tip ratio underground gas storage compressor stages[J]. Fluid Machinery, 2025 , 53 (7) : 61 -68 . DOI: 10.3969/j.issn.1005-0329.2025.07.009
Year 2025 volume 53 Issue 7
66
21
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doi: 10.3969/j.issn.1005-0329.2025.07.009
  • Receive Date:2024-12-25
  • Online Date:2026-10-20
  • Published:2025-07-30
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  • Received:2024-12-25
  • Revised:2025-04-17
Affiliations
    ShenGu Group Co.,Ltd.,Shenyang 110869,China
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
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Percentage of
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Genus
种数
Number of
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Percentage of total
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鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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